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Airfoil / Pitching moment / Lift coefficient / Disk loading / Turbine / Helicopter / Stall / Blade pitch / Helicopter rotor / Aerodynamics / Aerospace engineering / Fluid dynamics
Date: 2010-01-06 16:42:34
Airfoil
Pitching moment
Lift coefficient
Disk loading
Turbine
Helicopter
Stall
Blade pitch
Helicopter rotor
Aerodynamics
Aerospace engineering
Fluid dynamics

4E3 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL EXPERIMENTAL

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Source URL: crgis.ndc.nasa.gov

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File Size: 1,30 MB

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